Under-actuated aerial vehicles in addition to providing significant advantages in terms of design efficiency pose a considerable challenge in identifying and formulating an effective control scheme. Strong coupling among different axes in addition to under-actuation results in configurations more suited to unconventional design methodologies. This work presents a dynamic inversion based nonlinear control for an under-actuated glide vehicle designed with an inverted-V tail. The complexity of the problem is compounded by the fact that the platform comprises of only two control surfaces with the absence of any other input. Dynamic inversion has been applied to develop an effective stabilization scheme ensuring the stability of internal dynamics as well as to achieve limited decoupling among the axes in a high-fidelity environment. A single loop configuration has been utilized for this research which aims to stabilize the platform using controlled variables by direct utilization of states or state errors. A full scale six-DOF nonlinear mathematical model for the configuration, developed through CFD simulations, has been used for analysis and simulations to ensure accurate analysis of the effectiveness of the designed control law.